Abstract
The analysis and design procedure of an antenna for a cw doppler radar system being developed for pilot warning of midair collision hazards is presented. The antenna consists of two vertical arrays of half- wavelength dipoles mounted near a circular conducting cylinder. Each array provides relatively uniform illumination (2 to 3 db) in the forward 180//0 angular segment of the horizontal plane and approximately plus or minus 10 to 15//0 coverage in the vertical plane.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 960-967 |
| Number of pages | 8 |
| Journal | IEEE Transactions on Aerospace and Electronic Systems |
| Volume | AES-7 |
| Issue number | 5 |
| State | Published - Sep 1971 |
| Externally published | Yes |
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ASJC Scopus subject areas
- Computer Networks and Communications
- Aerospace Engineering
- Electrical and Electronic Engineering
Cite this
Analysis and design of antennas for air traffic collision avoidance systems. / BALANIS CA, CA; Balanis, Constantine.
In: IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-7, No. 5, 09.1971, p. 960-967.Research output: Contribution to journal › Article
}
TY - JOUR
T1 - Analysis and design of antennas for air traffic collision avoidance systems
AU - BALANIS CA, CA
AU - Balanis, Constantine
PY - 1971/9
Y1 - 1971/9
N2 - The analysis and design procedure of an antenna for a cw doppler radar system being developed for pilot warning of midair collision hazards is presented. The antenna consists of two vertical arrays of half- wavelength dipoles mounted near a circular conducting cylinder. Each array provides relatively uniform illumination (2 to 3 db) in the forward 180//0 angular segment of the horizontal plane and approximately plus or minus 10 to 15//0 coverage in the vertical plane.
AB - The analysis and design procedure of an antenna for a cw doppler radar system being developed for pilot warning of midair collision hazards is presented. The antenna consists of two vertical arrays of half- wavelength dipoles mounted near a circular conducting cylinder. Each array provides relatively uniform illumination (2 to 3 db) in the forward 180//0 angular segment of the horizontal plane and approximately plus or minus 10 to 15//0 coverage in the vertical plane.
UR - http://www.scopus.com/inward/record.url?scp=0015127094&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0015127094&partnerID=8YFLogxK
M3 - Article
VL - AES-7
SP - 960
EP - 967
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
SN - 0018-9251
IS - 5
ER -